A future geosynchronous space station will be used to collect solar energy. The energy is transmitted back to earth as an electromagnetic beam. The beam has a cross sectional area of 12.5m^2 and transmits an average power of 1.20 x 10^4 kW. What are the rms values of the electric of the and magnetic field of the beam? If the solar average power density is 1.4 kW/m^2, how large are the station's solar panels, assume 100% efficiency?